A feature of the Dove construction is the use of Redux to secure the stringers to the skin for parts of the fuselage, main plane, tail plane and fin with a single curvature. This process involves the application of controlled heat and pressure during construction, but normal repair methods can be applied to Reduxed members. Where there is double curvature the stringers are secured to the skin either by spot welding or riveting.


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    Title :

    Aircraft Engineering Reference Sheet


    Published in:

    Publication date :

    1949-09-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Aircraft Engineering Reference Sheet

    Tonkin, T. | Emerald Group Publishing | 1949


    Aircraft Engineering Reference Sheet

    Tonkin, T. | Emerald Group Publishing | 1949


    Aircraft Engineering Reference Sheet

    Tonkin, T. | Emerald Group Publishing | 1951


    Aircraft Engineering Reference Sheet

    Tonkin, T. | Emerald Group Publishing | 1950


    Aircraft Engineering Reference Sheet

    Tonkin, T. | Emerald Group Publishing | 1950